readAndAddSubscription uses nextDataMessage to find the first
corresponding data and nextDataMessage calls readAndAddSubscription
when it finds a new message definition.
* added optical flow to gz bridge
* log high rate sensor data
* it builds
* it builds and publishes, need to figure out build system now
* single library
* rename files
* add gz_msg for proto, fix build, test basic flow impl
* update rate, no blur
* PX4-OpticalFlow impl
* rename OpticalFlowSensor
* rename plugins
* disable gps, add plugin path
* cleanup
* fix plugin path export
* properly add OpticalFlowSystem dependency to gz
* move everything under gz_bridge
* cleanup
* add GZ_VEBOSE
* cleanup model/world build target cmake
* added GZ_DISTRO env, harmonic or ionic
* fix gz transport, unstage ark fpv bootloader
* unstage logged_topics.cpp
* cleanup
* make format
* ci fixes
* fix cmake
* remove required for gz-transport
* use model/world namespace for multi vehicle sim. Make format
* make format
* license
* remove needless member var
* made separate Kconfig for gz_msgs, gz_plugins, and gz_bridge
* move OpticalFlow build to it's own cmake
* fix clang
* cleanup comments
* fix rebase
* disable SENS_EN_GPSSIM for all gz airframes
* add GPS + noise to GZBridge
* remove mutex from gz callbacks. Callbacks run synchronously after sim update step and run() loop does not share resources.
* remove hrt check in callbacks
* format
* remove param set-default for already default params
* update submodule
* remove unnecessary comments
* overhaul of the GZBridge and px4-rc.simulator script
* remove arg
* shellcheck disable
* add bus/address
* start gz_bridge before adjusting sim speed or camera follow
Setting "lockdown" disables the actuators. In this mode,
"force_failsafe" has no effect as the actuators are disabled, so the
parachute is not getting released as it requires the output to change to
its failsafe value.
Previously, when requesting a mode switch to Position without a valid
position estimate through an RC button, the mode change to Position mode
was not rejected if COM_POSCTL_NAVL was set to 1 and instead the system
switched to Altitude mode.
If the mode request instead came in through MAVLink it was rejected.
This commit aligns the two ways of changing a flight mode.
Signed-off-by: Silvan <silvan@auterion.com>
We had a setup where the voltage was right at the threshold and the check
toggled continuously.
It still triggers immediately, and then keeps for 15 seconds
* add optical flow arming check
* removed deprecated mavlink_log_critical
* change SYS_HAS_NUM_OF description, keep max sensor at 1 since multiple instances are currently not support.
* restructure if/else blocks
Internal combustion engine control module.
New actuator functions and RPM based start/restart logic.
Not enabled by default.
---------
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
Co-authored-by: Pernilla <pernilla@auterion.com>
* Yawsticks on gimbal, vehicle follows gimbal in slowmode, once vehicle has taken off
* Increase queue length to avoid automatically unadvertise queued publications with queue length 1
* Improve readability
---------
Co-authored-by: Pernilla <pernilla@auterion.com>
Remove yaw_acceptance and altitude_acceptance_radius fields as they were only
filled by now removed avoidance controller.
Signed-off-by: Silvan <silvan@auterion.com>
* remove temp field from airspeed.msg, adjust temp selection
* temp-sensor hirarchy: airspeed, ext. baro, default value
* directly use diff-press or baro temp in true-airspeed calc
* improve clarity
* add enum for temperature source in VehicleAirData.msg
